View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 20804U 26110.82345587 +.00000000 +00000-0 +56650-4 0 00005
2 20804 82.9423 210.2890 0038166 79.0414 38.8963 13.74561280 09
| Epoch (UTC): | 20 April 2026 19:45:46 |
| Eccentricity: | 0.0038166 |
| inclination: | 82.9423° |
| perigee height: | 955 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 210.2890° |
| argument of perigee: | 79.0414° |
| revolutions per day: | 13.74561280 |
| mean anomaly at epoch: | 38.8963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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